View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 37223U 26032.27912828 +.00000000 +00000-0 +38999-3 0 00003
2 37223 71.9716 350.3797 0016291 293.0862 66.8594 14.99230841 02
| Epoch (UTC): | 01 February 2026 06:41:56 |
| Eccentricity: | 0.0016291 |
| inclination: | 71.9716° |
| perigee height: | 558 km |
| apogee height: | 581 km |
| right ascension of ascending node: | 350.3797° |
| argument of perigee: | 293.0862° |
| revolutions per day: | 14.99230841 |
| mean anomaly at epoch: | 66.8594° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|